Equations And Charts For The Evaluation Of The Hypersonic Aerodynamic Characteristics Of Lifting Configurations By The Newtonian Theory PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Equations And Charts For The Evaluation Of The Hypersonic Aerodynamic Characteristics Of Lifting Configurations By The Newtonian Theory PDF full book. Access full book title Equations And Charts For The Evaluation Of The Hypersonic Aerodynamic Characteristics Of Lifting Configurations By The Newtonian Theory.
| Author | : E. L. Clark |
| Publisher | : |
| Total Pages | : 98 |
| Release | : 1964 |
| Genre | : Aerodynamic load |
| ISBN | : |
Download Equations and Charts for the Evaluation of the Hypersonic Aerodynamic Characteristics of Lifting Configurations by the Newtonian Theory Book in PDF, ePub and Kindle
The pressure distribution predicted by the modified Newtonian theory is used to develop equations for the aerodynamic forces, moments, and stability derivatives for components of hypersonic lifting configurations. In conjunction with the equations, a set of charts is presented to enable simple determination of the aerodynamic characteristics of swept cylinders, swept wedges, spherical segments, and cone frustums at zero sideslip and angles of attack from 0 to 180 degrees. This method allows evaluation of most delta wing-body combinations without the need for numerical or graphical integration. As an example of the procedure, the theoretical characteristics of a blunt 75-degree swept delta wing are calculated and compared with experimental results.
| Author | : |
| Publisher | : |
| Total Pages | : 2180 |
| Release | : 1964 |
| Genre | : |
| ISBN | : |
Download U.S. Government Research Reports Book in PDF, ePub and Kindle
| Author | : |
| Publisher | : |
| Total Pages | : 1008 |
| Release | : 1978 |
| Genre | : Aeronautics |
| ISBN | : |
Download Scientific and Technical Aerospace Reports Book in PDF, ePub and Kindle
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
| Author | : Cornell Aeronautical Laboratory |
| Publisher | : |
| Total Pages | : 320 |
| Release | : 1967 |
| Genre | : Gas flow |
| ISBN | : |
Download Study of High-density Hypervelocity Flows and Similitudes Book in PDF, ePub and Kindle
| Author | : William R. Wells |
| Publisher | : |
| Total Pages | : 312 |
| Release | : 1962 |
| Genre | : Aerodynamics |
| ISBN | : |
Download Tables of Aerodynamic Coefficients Obtained from Developed Newtonian Expressions for Complete and Partial Conic and Spheric Bodies at Combined Angles of Attack and Sideslip with Some Comparisons with Hypersonic Experimental Data Book in PDF, ePub and Kindle
Newtonian closed-form expressions for the aerodynamic coefficients are developed for complete and partial conic and spheric bodies at combined angles of attack and sideslip. Calculations from these expressions are presented in tabulated form for various body shapes. Closed-form expressions for some of the static stability derivatives are also presented. Comparisons of this theory with hypersonic experimental data are made for many of the body shapes.
| Author | : Lewis R. Fisher |
| Publisher | : |
| Total Pages | : 38 |
| Release | : 1959 |
| Genre | : Aerodynamics |
| ISBN | : |
Download Equations and Charts for Determining the Hypersonic Stability Derivatives of Combinations of Cone Frustums Computed by Newtonian Impact Theory Book in PDF, ePub and Kindle
| Author | : |
| Publisher | : |
| Total Pages | : 62 |
| Release | : 1964 |
| Genre | : |
| ISBN | : |
Download Hypersonic Aerodynamic Characteristics of Four Series of Blunt Lifting Body and Winged Reentry Configurations Book in PDF, ePub and Kindle
| Author | : Walter B. Olstad |
| Publisher | : |
| Total Pages | : 70 |
| Release | : 1962 |
| Genre | : Aerodynamic load |
| ISBN | : |
Download Theoretical Evaluation of Hypersonic Forces, Moments, and Stability Derivatives for Combinations of Flat Plates, Including Effects of Blunt Leading Edges, by Newtonian Impact Theory Book in PDF, ePub and Kindle
| Author | : |
| Publisher | : |
| Total Pages | : 1016 |
| Release | : 1959 |
| Genre | : Aerodynamics |
| ISBN | : |
Download NASA Technical Report Book in PDF, ePub and Kindle
| Author | : |
| Publisher | : |
| Total Pages | : 758 |
| Release | : 2002 |
| Genre | : Aeronautics |
| ISBN | : |
Download The Aeronautical Journal Book in PDF, ePub and Kindle
